General specification for turbojet engines of missile
1 Scope
This specification specifies the general requirements, quality assurance requirements and delivery preparation of turbojet engines of missile.
This specification is applicable to the design, test, inspection and acceptance of turbojet engines of missile (hereinafter referred to as “engines”).
2 Normative references
The following documents contain provisions which, through reference in this text, constitute provisions of this code. For dated reference, subsequent amendments to (excluding any corrigendum), or revisions of, any of these publications do not apply. However, parties to agreements based on this specification are encouraged to investigate the possibility of applying the most recent editions of the documents indicated below. For undated references, the latest edition of the normative document referred to applies.
GB 1920-1980 Standard atmosphere (below 30 kilometers)
GJB 152A-1997 Measurement of electromagnetic emission and susceptibility requirements for military equipment and subsystems
GJB 241-1987 General specification for aircraft turbojet and turbofan engines
GJB 450-1988 General reliability program for materiel development and production
GJB 2103A-1997 Aircraft gas turbine powerplant terminology and symbols
QJ 1184.5-1987 Environmental specification for coastal defense missiles - Damp-heat test of missile equipment
QJ 1184.6-1987 Environmental specification for coastal defense missiles - Fungus test of missile equipment
QJ 1184.7-1987 Environmental specification for coastal defense missiles - Salt spray test of missile equipment
QJ 1184.8-1987 Environmental specification for coastal defense missiles - Impact test of missile equipment
QJ 1184.9-1987 Environmental specification for coastal defense missiles - Collision test of missile equipment
QJ 1184.10-1987 Environmental specification for coastal defense missiles - Bumping test of missile equipment
QJ 1184.11-1987 Environmental specification for coastal defense missiles - Acceleration test of missile equipment
QJ 1184.12-1987 Environmental specification for coastal defense missiles - Vibration test of missile equipment
QJ 2140A-1997 High altitude simulation test method of turbojet engines of missile
QJ 2744-1995 Ground static test method of turbojet engines of missile
3 Requirements
3.1 Dimension
The length, maximum outer diameter and maximum overall dimension of the engine (including engine accessories installed on the engine) shall meet the requirements of the development assignment or contract.
3.2 Weight
3.2.1 Dry weight
The dry weight of engine (i.e., the weight of engine without fuel and lubricating oil) shall meet the requirements of the development assignment or contract.
3.2.2 Weight of remaining liquid
When discharging the liquid in engine after operation, the weight of liquid remaining in the engine shall meet the requirements of the development assignment or contract.
3.3 Center of gravity
General specification for turbojet engines of missile
1 Scope
This specification specifies the general requirements, quality assurance requirements and delivery preparation of turbojet engines of missile.
This specification is applicable to the design, test, inspection and acceptance of turbojet engines of missile (hereinafter referred to as “engines”).
2 Normative references
The following documents contain provisions which, through reference in this text, constitute provisions of this code. For dated reference, subsequent amendments to (excluding any corrigendum), or revisions of, any of these publications do not apply. However, parties to agreements based on this specification are encouraged to investigate the possibility of applying the most recent editions of the documents indicated below. For undated references, the latest edition of the normative document referred to applies.
GB 1920-1980 Standard atmosphere (below 30 kilometers)
GJB 152A-1997 Measurement of electromagnetic emission and susceptibility requirements for military equipment and subsystems
GJB 241-1987 General specification for aircraft turbojet and turbofan engines
GJB 450-1988 General reliability program for materiel development and production
GJB 2103A-1997 Aircraft gas turbine powerplant terminology and symbols
QJ 1184.5-1987 Environmental specification for coastal defense missiles - Damp-heat test of missile equipment
QJ 1184.6-1987 Environmental specification for coastal defense missiles - Fungus test of missile equipment
QJ 1184.7-1987 Environmental specification for coastal defense missiles - Salt spray test of missile equipment
QJ 1184.8-1987 Environmental specification for coastal defense missiles - Impact test of missile equipment
QJ 1184.9-1987 Environmental specification for coastal defense missiles - Collision test of missile equipment
QJ 1184.10-1987 Environmental specification for coastal defense missiles - Bumping test of missile equipment
QJ 1184.11-1987 Environmental specification for coastal defense missiles - Acceleration test of missile equipment
QJ 1184.12-1987 Environmental specification for coastal defense missiles - Vibration test of missile equipment
QJ 2140A-1997 High altitude simulation test method of turbojet engines of missile
QJ 2744-1995 Ground static test method of turbojet engines of missile
3 Requirements
3.1 Dimension
The length, maximum outer diameter and maximum overall dimension of the engine (including engine accessories installed on the engine) shall meet the requirements of the development assignment or contract.
3.2 Weight
3.2.1 Dry weight
The dry weight of engine (i.e., the weight of engine without fuel and lubricating oil) shall meet the requirements of the development assignment or contract.
3.2.2 Weight of remaining liquid
When discharging the liquid in engine after operation, the weight of liquid remaining in the engine shall meet the requirements of the development assignment or contract.
3.3 Center of gravity
